Experimental Study of Downstream Combustion Ramjet-Mode

Author:

Kato Kanenori1,Kanda Takeshi1,Kobayashi Kan1,Kudo Kenji1,Murakami Atsuo1

Affiliation:

1. Japan Aerospace Exploration Agency

Publisher

American Institute of Aeronautics and Astronautics

Cited by 5 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Experimental study on ejector-to-ramjet mode transition in a divergent kerosene-fueled RBCC combustor with low total temperature inflow;Aerospace Science and Technology;2020-04

2. Experimental investigation of isolated inlets for high agile missiles;Aerospace Science and Technology;2006-12

3. Experimental Study of a Combined-Cycle Engine Combustor in Ejector-Jet Mode;44th AIAA Aerospace Sciences Meeting and Exhibit;2006-01-09

4. Pressure Distribution Measurements in Scramjet Isolators under Asymmetric Supersonic Flow;44th AIAA Aerospace Sciences Meeting and Exhibit;2006-01-09

5. Design of Sub-scale Rocket-Ramjet Combined Cycle E...;56th International Astronautical Congress of the International Astronautical Federation, the International Academy of Astronautics, and the International Institute of Space Law;2005-10-17

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